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A turbomachine includes a compressor having an intake portion and an outlet portion. The compressor compresses air received at the intake portion to form a compressed airflow that is passed from the outlet portion. The turbomachine also includes an intercooler operatively connected downstream from t

A turbomachine includes a compressor having an intake portion and an outlet portion. The compressor compresses air received at the intake portion to form a compressed airflow that is passed from the outlet portion. The turbomachine also includes an intercooler operatively connected downstream from the compressor. The intercooler includes a plurality of heat pipes that are configured to extract heat from the compressed airflow.

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1. A turbomachine comprising: a compressor including an intake portion and an outlet portion, the compressor compressing air received at the intake portion to form a compressed airflow passed from the outlet portion; andan intercooler operatively connected downstream of the compressor, the intercool

1. A turbomachine comprising: a compressor including an intake portion and an outlet portion, the compressor compressing air received at the intake portion to form a compressed airflow passed from the outlet portion; andan intercooler operatively connected downstream of the compressor, the intercooler including a plurality of heat pipes configured to extract heat from the compressed airflow, each of the plurality of heat pipes being sealed, having a partial vacuum, and including a working fluid at least a portion of which is in a liquid phase and another portion of which is in a gas phase. 2. The turbomachine according to claim 1, wherein the intercooler includes a pressure vessel, each of the plurality of heat pipes including a first end portion extending into the pressure vessel and a second end portion projecting out from the pressure vessel. 3. The turbomachine according to claim 2, further comprising: at least one fan directed at the intercooler, the at least one fan directing a forced airflow over the second end portion of each of the plurality of heat pipes. 4. The turbomachine according to claim 1, wherein at least a portion of the plurality of heat pipes are hermetically sealed heat pipes that include a coolant in at least one of a liquid phase and a vapor phase. 5. The turbomachine according to claim 1, wherein each of the plurality of heat pipes includes an external surface and an internal surface, at least a portion of the plurality of heat pipes including a heat conductive coating on the internal surface. 6. The turbomachine according to claim 1, further comprising: another compressor arranged downstream from the intercooler, the another compressor further compressing the compressed airflow passing from the intercooler. 7. The turbomachine according to claim 1, wherein the intercooler does not include water as a coolant. 8. A method of extracting heat from a compressed airflow generated by a turbomachine, the method comprising: passing an airflow to a compressor, the compressor acting on the airflow to create a compressed airflow at a first temperature;guiding the compressed airflow at the first temperature from the compressor to an intercooler having a plurality of heat pipes, each of the plurality of heat pipes being sealed, having a partial vacuum, and including a working fluid at least a portion of which is in a liquid phase and another portion of which is in a gas phase;passing the compressed airflow over the plurality of heat pipes, the heat pipes absorbing heat from the compressed airflow to establish a compressed airflow at a second temperature, the second temperature being less that the first temperature. 9. The method of claim 8, further comprising: passing the compressed airflow into a pressure vessel, each of the plurality of heat pipes including a first end portion extending into the pressure vessel and a second end portion projecting out from the pressure vessel. 10. The method of claim 9, further comprising: passing a convective airflow over the second end portion of each of the plurality of heat pipes. 11. The method of claim 8, further comprising: passing the compressed airflow at the second temperature into a turbine. 12. The method of claim 8, further comprising: passing the compressed airflow at the second temperature to another compressor, the another compressor further compressing the compressed airflow to create a further compressed airflow at a third temperature, the third temperature being higher than the second temperature. 13. The method of claim 12, further comprising: passing the further compressed airflow to a turbine. 14. An intercooler operatively connected downstream from a compressor, the intercooler comprising: a plurality of heat pipes configured to extract heat from a compressed airflow and pass the compressed airflow, each of the plurality of heat pipes being sealed, having a partial vacuum, and including a working fluid at least a portion of which is in a liquid phase and another portion of which is in a gas phase. 15. The intercooler according to claim 14, wherein the intercooler includes a pressure vessel, each of the plurality of heat pipes including a first end portion extending into the pressure vessel that leads to a second end portion projecting out from the pressure vessel. 16. The intercooler according to claim 15, further comprising: at least on fan directed at the intercooler, the at least one fan directing a forced airflow over the second end portion of each of the plurality of heat pipes. 17. The intercooler according to claim 14, wherein at least a portion of the plurality of heat pipes are hermetically sealed heat pipes that include a coolant in at least one of a liquid phase and a vapor phase. 18. The intercooler according to claim 14, wherein each of the plurality of heat pipes includes an external surface and an internal surface, at least a portion of the plurality of heat pipes include a heat conductive coating on the internal surface. 19. The intercooler according to claim 14, wherein the intercooler does not include water as a coolant. 20. The intercooler according to claim 14, wherein the intercooler is fluidly connected to a turbine.